Optimal fuel consumption trajectories of a civil supersonic aircraftстатьяИсследовательская статья
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Дата последнего поиска статьи во внешних источниках: 30 января 2024 г.
Аннотация:The optimal fuel consumption trajectories of a supersonic passenger aircraft are constructed. A mathematical model of an airliner, which describes in detail the properties of the devicerelated to the design characteristics of the aircraft, is applied. For optimization, the preliminary division of the trajectory into separate sections followed by the assembly of the optimal solution from them is not used. The whole flight is considered as a single process. The classical method of dynamic programming is used for the calculations.